
CS 3a (Sakura 3a)
| Nation: | Japan |
|---|---|
| Type / Application: | Communication |
| Operator: | |
| Contractors: | Mitsubishi Electric |
| Equipment: | 2 (+1) C-band transponders 4W TWTA, 180 MHz bandwidth, EIRP max 29 dBW 10 (+5) Ka-band transponders 4.2W TWTA, 100 MHz bandwidth, EIRP max 37 dBW |
| Configuration: | |
| Propulsion: | Star-30B |
| Power: | Solar cells, batteries |
| Lifetime: | |
| Mass: | |
| Orbit: | GEO |
| Satellite | Date | LS | Launch Vehicle | Remarks | |
|---|---|---|---|---|---|
| CS 3a (Sakura 3a) | 19.02.1988 | Ta | H-1 UM-129A (9 SO) | ||
| CS 3b (Sakura 3b) | 16.09.1988 | Ta | H-1 UM-129A (9 SO) |